LIVE$APIEDCA0x720800690cd81c3319cb0ab9c4f480b659a772d4
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space.halowerk.com

Uses da/dt = -rho×sqrt(mu×a)/ballistic_coefficient for a circular orbit, holds density and ballistic coefficient constant, and linearly projects altitude over a bounded horizon. Real density changes rapidly with altitude and solar activity; the result is not a lifetime prediction or maneuver plan.

space.halowerk.comBase last paid 25d ago
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Other services
Starting price
$0.002
Paid calls · 30 days
25
Unique payers · 30 days
25

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